CN204992867U - A motor cabinet for on multiaxis aircraft - Google Patents
A motor cabinet for on multiaxis aircraft Download PDFInfo
- Publication number
- CN204992867U CN204992867U CN201520809044.9U CN201520809044U CN204992867U CN 204992867 U CN204992867 U CN 204992867U CN 201520809044 U CN201520809044 U CN 201520809044U CN 204992867 U CN204992867 U CN 204992867U
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- motor
- mounting groove
- circuit board
- control circuit
- lower house
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Abstract
The utility model relates to a many rotor unmanned aerial vehicle part, concretely relates to a motor cabinet for on multiaxis aircraft, including last casing and lower casing, to go up the casing and be equipped with a semicircle portion that corresponds of each other respectively on the casing down, two semicircle portions form a clamping part, still are equipped with the motor mounting groove on going up the casing, are equipped with the control circuit board mounting groove on the lower casing, and under the control circuit board mounting groove lay in the motor mounting groove, motor mounting groove bottom was equipped with the motor and holds in the palm, and the motor holds in the palm and separates motor mounting groove and control circuit board mounting groove, is equipped with the mounting hole that is used for installing the motor in the motor support, the junction of going up casing and lower casing is equipped with crashproof rubber, and the last casing and the inferior valve body coupling department of crashproof rubber both sides are equipped with the lamp shade, lower casing bottom still be equipped with the louvre. The utility model discloses on also installing the motor cabinet with control circuit board to realize control circuit board and motor control effect one to one, have the effect of anticollision, also can play the effect of location during night flight.
Description
Technical field
The utility model relates to a kind of Multi-axis aircraft parts, is specifically related to a kind of motor cabinet on Multi-axis aircraft.
Background technology
Multi-axis aircraft, i.e. many rotor wing unmanned aerial vehicles, be provided with multiple screw, flight is realized by the multiple screw of multiple Electric Machine Control, be widely used in take photo by plane, monitor, search and rescue, the every field such as resource exploration, agricultural, have that volume is little, lightweight, expense is low, flexible operation and a fail safe high.Multi-axis aircraft has more horn, Multi-axis aircraft provide the motor of power to be mostly arranged on the outer end of horn to screw, motor is all generally be arranged on horn by motor cabinet, motor cabinet of the prior art is just for mounted motor, there is no other functions, and the circuit board controlling motor can not be arranged on motor cabinet, need to install separately in addition, extremely bother.
Summary of the invention
The utility model is for motor cabinet function singleness in prior art, troublesome drawback installed by motor, a kind of motor cabinet on Multi-axis aircraft is provided, motor cabinet of the present utility model is divided into upper shell and lower house two parts, motor can be made to become and to be more prone to install, and motor holder is set on upper shell, thus the hole of script mounted motor is divided into motor mounting groove and control circuit board mounting groove, make motor and control the circuit board of motor to be arranged on motor cabinet simultaneously and separate independence and install, do not interfere with each other, be provided with anti-collision rubber in motor cabinet side simultaneously, the effect of cushion bumper is played when may touch external object in Multi-axis aircraft flight course.
Goal of the invention of the present utility model is achieved through the following technical solutions: a kind of motor cabinet on Multi-axis aircraft, comprise upper shell and lower house, upper shell and lower house are respectively equipped with a half-round in correspondence with each other, two half-round form one for clamping the clamping part of horn, upper shell is also provided with the motor mounting groove for mounted motor, lower house is provided with the control circuit board mounting groove installing control circuit board, control circuit board mounting groove is positioned at immediately below motor mounting groove, motor holder is provided with bottom motor mounting groove, motor mounting groove and control circuit board mounting groove separate by motor holder, motor holder is provided with the installing hole for mounted motor, the junction of upper shell and lower house is provided with anti-collision rubber, upper shell and the lower house junction of anti-collision rubber both sides are provided with lampshade, inside lampshade, can small lamp bulb be set, the light that small lamp bulb can distribute by lampshade is thoroughly to outside, play the effect of location when Multi-axis aircraft night flying, flight effect is also more gorgeous, some louvres are also provided with bottom described lower house.
As preferably, described motor holder is the platy structure of " X " shape.Motor mounting groove and control circuit board mounting groove separate by motor holder, motor holder is set to the platy structure of " X " shape, hole motor holder having through motor mounting groove and control circuit board mounting groove can be made, can be used in this some holes the electric wire connecting motor is installed.
As preferably, the center of motor holder is provided with axis hole.The rotating shaft of motor is all the head and the tail two ends running through motor, and when motor is arranged in motor holder, the rotating shaft of stretching out from motor tail end can be arranged in axis hole, and such arranging can make motor vertically be arranged in motor holder, and rotating shaft can not impact installation site.
As preferably, the junction of upper shell and lower house is provided with some square grooves.By groove, anti-collision rubber and lampshade can be set.The installation of anti-collision rubber and lampshade is made to become detachable.
As preferably, described anti-collision rubber cross section is " work " character form structure, and the anti-collision rubber of " work " character form structure can embed in square groove.The anti-collision rubber of " work " character form structure and the setting of square groove, make to become demountable structure between anti-collision rubber and upper and lower casing, and what make anti-collision rubber removes and installs the very convenient of change, and it is more convenient to change.
As preferably, described lampshade cross section is " work " character form structure, and the lampshade of " work " character form structure can embed in square groove.The lampshade of " work " character form structure can embed in square groove.The lampshade of " work " character form structure and the setting of square groove, make to become demountable structure between lampshade and upper and lower casing, and what make lampshade removes and installs the very convenient of change, and it is more convenient to change.
As preferably, upper shell and lower house being all provided with some installation screws in correspondence with each other, by arranging bolt in installation screw, upper shell and lower house being linked together.Motor cabinet is divided into upper and lower casing two parts, makes the installation of motor and control circuit board become easy.
Compared with prior art, the utility model has following beneficial effect: motor cabinet of the present utility model is divided into upper shell and lower house two parts, motor can be made to become and to be more prone to install, and motor holder is set on upper shell, thus the hole of script mounted motor is divided into motor mounting groove and control circuit board mounting groove, make motor and control the circuit board of motor to be arranged on motor cabinet simultaneously and can separate independence and install, do not interfere with each other; The anti-collision rubber arranged in motor cabinet side, the effect of cushion bumper is played when touching external object in Multi-axis aircraft flight course, reduce damage, the light that small lamp bulb inside lampshade can distribute by the lampshade arranged in motor cabinet side is thoroughly to outside, play the effect of location when Multi-axis aircraft night flying, flight effect is also more gorgeous.
In sum, the control circuit board controlling motor can also be installed on motor cabinet by the utility model, thus realizes control circuit board and the man-to-man control effects of motor; And have crashproof effect, the effect of location also can be played when night flying.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Fig. 2 is the utility model explosive view;
Fig. 3 is the utility model using state figure;
Mark in figure: 1, upper shell, 2, lower house, 3, half-round, 4, clamping part, 5, motor mounting groove, 6, control circuit board mounting groove, 7, motor holder, 8, installing hole, 9, anti-collision rubber, 10, lampshade, 11, louvre, 12, axis hole, 13, square groove, 14, installation screw, 15, motor, 16, control circuit board.
Embodiment
Below in conjunction with the embodiment represented by accompanying drawing 1-3, the utility model is further described:
Embodiment 1
As Figure 1-3, a kind of motor cabinet on Multi-axis aircraft, comprise upper shell 1 and lower house 2, upper shell 1 and lower house 2 are respectively equipped with a half-round 3 in correspondence with each other, two half-round 3 form one for clamping the clamping part 4 of horn, upper shell 1 is also provided with motor mounting groove 5, lower house 2 is provided with the control circuit board mounting groove 6 installing control circuit board 16, control circuit board mounting groove 6 is positioned at immediately below motor mounting groove 5, the motor holder 7 of " X " shape platy structure is provided with bottom motor mounting groove 5, motor mounting groove 5 and control circuit board mounting groove 6 separate by motor holder 7, motor holder 7 is provided with the installing hole 8 for mounted motor 15, upper shell 1 is provided with three square grooves 13 with the junction of lower house 2.Middle square groove 13 is provided with the anti-collision rubber 9 of cross section for " work " character form structure, and the direction groove 13 of anti-collision rubber 9 both sides is all provided with the lampshade 10 that a cross section is " work " character form structure, is also provided with louvre 11 bottom described lower house 2.
The center of motor holder 7 is also provided with axis hole 12.The rotating shaft of motor 15 is all the head and the tail two ends running through motor 15, when motor 15 is arranged in motor holder 7, the rotating shaft of stretching out from motor 15 tail end can be arranged in axis hole 12, and such arranging can make motor 15 vertically be arranged in motor holder 7, and rotating shaft can not impact installation site.
Upper shell 1 and lower house 2 being all provided with six installation screws 14 in correspondence with each other, by arranging bolt in installation screw 14, upper shell 1 and lower house 2 being linked together.And motor cabinet is divided into upper and lower casing two parts, make the installation of motor 15 and control circuit board become easy.
Specific embodiment described in literary composition is only to the explanation for example of the utility model spirit.The utility model person of ordinary skill in the field can make various amendment or supplements or adopt similar mode to substitute to described specific embodiment, but can't depart from spirit of the present utility model or surmount the scope that appended claims defines.
Claims (7)
1. the motor cabinet on Multi-axis aircraft, comprise upper shell (1) and lower house (2), upper shell and lower house are respectively equipped with a half-round (3) in correspondence with each other, two half-round form one for clamping the clamping part (4) of horn, it is characterized in that, upper shell is also provided with motor mounting groove (5), lower house is provided with control circuit board mounting groove (6), control circuit board mounting groove is positioned at immediately below motor mounting groove, motor holder (7) is provided with bottom motor mounting groove, motor mounting groove and control circuit board mounting groove separate by motor holder, motor holder is provided with the installing hole (8) for mounted motor, the junction of upper shell and lower house is provided with anti-collision rubber (9), and the upper shell of anti-collision rubber both sides and lower house junction are provided with lampshade (10), some louvres (11) are also provided with bottom described lower house.
2. a kind of motor cabinet on Multi-axis aircraft according to claim 1, is characterized in that, described motor holder is the platy structure of " X " shape.
3. a kind of motor cabinet on Multi-axis aircraft according to claim 1 and 2, is characterized in that, the center of motor holder is provided with axis hole (12).
4. a kind of motor cabinet on Multi-axis aircraft according to claim 1 and 2, is characterized in that, the junction of upper shell and lower house is provided with some square grooves (13).
5. a kind of motor cabinet on Multi-axis aircraft according to claim 4, is characterized in that, described anti-collision rubber cross section is " work " character form structure, and the anti-collision rubber of " work " character form structure can embed in square groove.
6. a kind of motor cabinet on Multi-axis aircraft according to claim 4, is characterized in that, described lampshade cross section is " work " character form structure, and the lampshade of " work " character form structure can embed in square groove.
7. a kind of motor cabinet on Multi-axis aircraft according to claim 1, it is characterized in that, upper shell and lower house being all provided with some installation screws (14) in correspondence with each other, by arranging bolt in installation screw, upper shell and lower house being linked together.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520809044.9U CN204992867U (en) | 2015-10-20 | 2015-10-20 | A motor cabinet for on multiaxis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520809044.9U CN204992867U (en) | 2015-10-20 | 2015-10-20 | A motor cabinet for on multiaxis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204992867U true CN204992867U (en) | 2016-01-20 |
Family
ID=55127192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520809044.9U Expired - Fee Related CN204992867U (en) | 2015-10-20 | 2015-10-20 | A motor cabinet for on multiaxis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204992867U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106505775A (en) * | 2016-12-08 | 2017-03-15 | 中国科学院长春光学精密机械与物理研究所 | A kind of motor cabinet of effective radiating |
| CN107031813A (en) * | 2016-02-04 | 2017-08-11 | 顺丰科技有限公司 | Multi-rotor unmanned aerial vehicle frame central part |
| CN107031831A (en) * | 2016-11-21 | 2017-08-11 | 芜湖万户航空航天科技有限公司 | Depopulated helicopter motor fixing device |
| WO2018086225A1 (en) * | 2016-11-08 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Power device, and unmanned aerial vehicle |
| CN109661762A (en) * | 2017-01-06 | 2019-04-19 | 深圳市大疆创新科技有限公司 | Motor, power device, power suit and aircraft |
-
2015
- 2015-10-20 CN CN201520809044.9U patent/CN204992867U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107031813A (en) * | 2016-02-04 | 2017-08-11 | 顺丰科技有限公司 | Multi-rotor unmanned aerial vehicle frame central part |
| WO2018086225A1 (en) * | 2016-11-08 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Power device, and unmanned aerial vehicle |
| CN107031831A (en) * | 2016-11-21 | 2017-08-11 | 芜湖万户航空航天科技有限公司 | Depopulated helicopter motor fixing device |
| CN107031831B (en) * | 2016-11-21 | 2019-10-29 | 芜湖万户航空航天科技有限公司 | Unmanned helicopter motor fixing device |
| CN106505775A (en) * | 2016-12-08 | 2017-03-15 | 中国科学院长春光学精密机械与物理研究所 | A kind of motor cabinet of effective radiating |
| CN109661762A (en) * | 2017-01-06 | 2019-04-19 | 深圳市大疆创新科技有限公司 | Motor, power device, power suit and aircraft |
| CN109661762B (en) * | 2017-01-06 | 2021-07-27 | 深圳市大疆创新科技有限公司 | Motor, power device, power suit and aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201130 Address after: No.29, Fuhou Road, Funan Economic Development Zone, Fuyang City, Anhui Province Patentee after: Anhui Zhitian Intelligent Technology Co.,Ltd. Address before: 321000, south wing, room 520, building 1111, Li Yu East Road, Jindong District, Zhejiang, Jinhua Patentee before: ZHEJIANG ZHITIAN TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160120 Termination date: 20211020 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |